TW201938899A - Shield tail clearance measuring device and shield shell capable of preventing a base portion from protrusion out of an inner peripheral surface of the shield - Google Patents

Shield tail clearance measuring device and shield shell capable of preventing a base portion from protrusion out of an inner peripheral surface of the shield Download PDF

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TW201938899A
TW201938899A TW107109816A TW107109816A TW201938899A TW 201938899 A TW201938899 A TW 201938899A TW 107109816 A TW107109816 A TW 107109816A TW 107109816 A TW107109816 A TW 107109816A TW 201938899 A TW201938899 A TW 201938899A
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Taiwan
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shield
measuring device
tunnel lining
rotary
shield tail
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TW107109816A
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Chinese (zh)
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TWI763805B (en
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吉田英典
森竜生
青山憲彦
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日商奧村組股份有限公司
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Abstract

A shield tail clearance measuring device (10) of the present invention includes a base portion (16), a rotating shaft portion (17) supported by the base portion (16), a rotation angle sensor (18), a hand contact portion (19) integrally joined with the rotating shaft portion (17), and a rotating elastic pushing mechanism (20) for providing a rotating elastic force to the hand contact portion (19). The rotating elastic pushing mechanism (20) includes a reversing mechanism (20a) for releasing the rotating elastic force to rotate the rotating shaft portion (17) in an opposite direction, and is configured to rotate the rotating shaft portion (17) in a manner of rotating the hand contact portion (19) toward the opposite side of the central axis of the shield shell (12), so as to accommodate the contact hand portion in the height range of the base portion (16).

Description

盾尾間隙測量裝置及盾殻Shield tail gap measuring device and shield shell

本發明係關於一種測量被保持於潛盾機之盾殻、與在該盾殻之後部組裝之環片之外周面之間的盾尾間隙之盾尾間隙測量裝置及盾殻。The present invention relates to a shield tail gap measuring device and a shield shell for measuring a shield tail gap between a shield case held by a submersible shield machine and an outer peripheral surface of a ring piece assembled at a rear portion of the shield case.

潛盾工法係如下之工藝:一面利用泥土、泥水、壓氣等壓抵潛盾機前端之切割端面一面利用切割器挖削地基,並且一面於潛盾機之後方組裝由環片構成之隧道襯砌體,一面自起始豎井朝向終點豎井於地中形成隧道;該工藝作為用於城市地區或平原地區之主要之隧道工程之工藝而被廣泛採用。 用於潛盾工法之潛盾機係於被稱為盾殻之金屬製之外殼體之前部具備切削挖掘面之旋轉切割器、或隔板、切割器驅動裝置、排土機構等,且於盾殻之後部具備推進千斤頂、安裝裝置等,使用安裝裝置組裝由環片構成之隧道襯砌體,自組裝而成之隧道襯砌體獲得反作用力,且藉由推進千斤頂一起推動盾殻及旋轉切割器,由此一面切削挖掘面一面鑽掘隧道。 又,於組裝而成之隧道襯砌體之外周面、與覆蓋其之後部之盾殻之內周面之間,保持被稱為盾尾間隙之間隙,藉此,於使潛盾機前進時,可在保留隧道襯砌體之狀態下使盾殻沿著隧道襯砌體之外周面順利地朝前方移動,於對曲線部分進行施工時,可利用保持之間隙,使盾殻相對於隧道襯砌體逐漸地朝彎曲之方向前進。進而,為了不使土砂或地下水經由盾尾間隙自周圍之地盤流入至潛盾機之內部,而於盾尾間隙將由例如具有可撓性之環狀構件構成之尾密封件於隧道襯砌體及盾殻之軸向上隔開間隔地安裝複數個。 另一方面,於此種潛盾機中,就例如防止因尾部中之隧道襯砌體與盾殻之干涉所致之環片之變形或破損,提高隧道襯砌體之品質而言,重要的是測量盾尾間隙之間隙量並掌握其變化。又,於對曲線部分進行施工時,為了能以計劃之角度變更前進路徑,重要的是將盾尾間隙之間隙量維持於特定之範圍內,且測量盾尾間隙之間隙量並掌握其變化。因此,提出各種測量盾尾間隙之裝置或方法(例如參照專利文獻1~6等)。 此處,專利文獻1記載之盾尾間隙測定裝置係藉由測量安裝在以抵接於環片之方式配置之彈推機構之金屬線之長度方向的移動量,而測量盾尾間隙之間隙量者,於專利文獻2記載之潛盾機中,藉由非接觸型之距離感測器測量盾尾間隙之間隙量。專利文獻3記載之盾尾間隙測定裝置係根據由距離感測器測量出之至環片之內周面之距離算出盾尾間隙之間隙量者,專利文獻4記載之盾尾間隙測量裝置係藉由超音波感測器檢測與接觸於盾殻之檢測器之間之距離,而算出盾尾間隙之間隙量者。專利文獻5記載之盾尾間隙之測定裝置係使用藉由距離感測器檢測出之該感測器至盾殻之內周面之距離、該感測器至環片之內周面之距離、及環片之厚度而運算盾尾間隙之間隙量者,專利文獻6記載之盾尾間隙測定方法係基於以CCD(Charge Couple Device:電荷耦合裝置)相機拍攝到之圖像資料,算出盾尾間隙之間隙量者。 [先前技術文獻] [專利文獻] [專利文獻1]日本專利特公平6-050036號公報 [專利文獻2]日本專利特公平6-102959號公報 [專利文獻3]日本專利特開平4-041895號公報 [專利文獻4]日本專利第2722032號公報 [專利文獻5]日本專利第3229409號公報 [專利文獻6]日本專利第6026974號公報 [專利文獻7]日本專利特開2015-45165號公報The submersible shield construction method is as follows: while using earth, mud water, gas, etc. to press against the cutting end face of the submersible shield machine, the cutter is used to dig the foundation, and the tunnel lining body composed of rings is assembled behind the submersible shield machine. One side forms a tunnel in the ground from the starting shaft to the ending shaft; this process is widely used as the main tunnel engineering process for urban or plain areas. The submersible shield machine used for the submersible shield construction method is a rotary cutter, or partition, cutter driving device, earth discharging mechanism, etc., which is provided with a cutting and digging surface at the front of a metal outer casing called a shield shell, and is used in the shield. The rear part of the shell is equipped with a pushing jack and a mounting device. The mounting device is used to assemble a tunnel lining body composed of ring pieces. The self-assembled tunnel lining body obtains a reaction force, and the shield shell and the rotary cutter are pushed together by the pushing jack. The tunnel is cut while cutting the digging surface. In addition, a gap called a shield tail gap is maintained between the outer peripheral surface of the assembled tunnel lining body and the inner peripheral surface of the shield shell covering the rear part of the tunnel lining body. The shield shell can be smoothly moved forward along the outer peripheral surface of the tunnel lining body while the tunnel lining body is retained. During the construction of the curved part, the remaining gap can be used to gradually make the shield shell relative to the tunnel lining body. Move in a curved direction. Furthermore, in order to prevent earth, sand or groundwater from flowing into the submersible shield from the surrounding site through the shield tail gap, a tail seal made of, for example, a flexible ring-shaped member at the shield tail gap is used in the tunnel lining and the shield. A plurality of shells are mounted at intervals in the axial direction. On the other hand, in this type of submersible shield machine, it is important to measure the quality of the tunnel lining body in order to prevent deformation or damage of the ring piece caused by the interference of the tunnel lining body and the shield shell in the tail, for example. The amount of gap in the shield tail gap and grasp its change. In addition, in order to change the forward path at a planned angle when constructing a curved portion, it is important to maintain the gap amount of the shield tail gap within a specific range, and measure the gap amount of the shield tail gap and grasp the change. Therefore, various devices or methods for measuring the gap of the shield tail have been proposed (for example, refer to Patent Documents 1 to 6). Here, the shield tail gap measuring device described in Patent Document 1 measures the amount of movement of the shield tail gap by measuring the amount of movement in the length direction of the metal wire mounted on the spring pushing mechanism arranged so as to abut the ring piece. In the submersible shield machine described in Patent Document 2, the gap amount of the shield tail gap is measured by a non-contact type distance sensor. The shield tail gap measuring device described in Patent Document 3 calculates the gap amount of the shield tail gap based on the distance measured from the distance sensor to the inner peripheral surface of the ring. The shield tail gap measurement device described in Patent Document 4 borrows The distance between the shield tail gap is calculated by the distance between the ultrasonic sensor and the detector in contact with the shield shell. The device for measuring the shield tail gap described in Patent Document 5 uses the distance from the sensor to the inner peripheral surface of the shield case detected by the distance sensor, the distance from the sensor to the inner peripheral surface of the ring, For the calculation of the gap between the shield tail and the thickness of the ring, the shield gap measurement method described in Patent Document 6 is based on the image data captured by a CCD (Charge Couple Device) camera to calculate the shield gap. The amount of clearance. [Prior Art Literature] [Patent Literature] [Patent Literature 1] Japanese Patent Publication No. 6-050036 [Patent Literature 2] Japanese Patent Publication No. 6-102959 [Patent Literature 3] Japanese Patent Publication No. 4-041895 Gazette [Patent Document 4] Japanese Patent No. 2722032 [Patent Document 5] Japanese Patent No. 3229409 [Patent Document 6] Japanese Patent No. 6026974 [Patent Document 7] Japanese Patent Laid-Open No. 2015-45165

於上述先前之測量盾尾間隙之裝置或方法中,因耐久性產生問題,或由於並非直接機械地測量間隙量,而難以準確地測量間隙量,故本案申請人於專利文獻7中,揭示有如下之盾尾間隙測量裝置及盾殻:可機械地連續測量盾尾間隙之間隙量,容易地掌握其變化,並且具備能長期間地配置於隧道襯砌體與盾殻之間之相當之耐久性,且亦可容易地進行更換作業。 然而,根據專利文獻7記載之盾尾間隙測量裝置或盾殻,以自盾殻之後方側接觸於環片之外周面之狀態配置之接觸手部係將彈簧部作為彈推機構,成為於測量中始終以朝向盾殻中心軸側旋動之方式被彈推之狀態,故如圖9(a)、(b)所示,若使盾殻52相對於隧道襯砌體51前進至安裝有盾尾間隙測量裝置50之部分超過組裝而成之隧道襯砌體51之前端,則接觸手部53因彈簧部之作用力而較隧道襯砌體51之外周面朝隧道襯砌體51之中心軸側凸出,而成為組裝下一個隧道襯砌體51時之阻礙,或有接觸手部53被夾於前端之隧道襯砌體51與下一個組裝而成之隧道襯砌體51之間而破損之虞。 因此,於先前之方法中,如圖9(c)所示,進行如下之研究:藉由使盾殻52之前進停留至安裝有盾尾間隙測量裝置50部分不超過組裝而成之隧道襯砌體51之前端之位置,於組裝下一個隧道襯砌體51時,接觸手部53不會因彈簧部之作用力而朝隧道襯砌體51之中心軸側凸出;但相應地,需要將盾殻52延長,故無法效率良好地進行施工,且組裝而成之隧道襯砌體51與盾殻52之後端部分重合之長度變長。若組裝而成之隧道襯砌體51與盾殻52之後端部分重合之長度變長,則尤其於對於急劇彎曲之曲線部分進行施工時會產生障礙,因此期望儘可能地縮短隧道襯砌體與盾殻之後端部分重合之長度。 本發明之目的在於提供一種盾尾間隙測量裝置及盾殻,其係即使盾殻相對於隧道襯砌體前進至安裝有測量裝置之部分超過組裝而成之隧道襯砌體之前端,接觸手部亦不會較隧道襯砌體之外周面朝隧道襯砌體之中心軸側凸出,不會成為組裝下一個隧道襯砌體時之阻礙,且可有效地抑制組裝而成之隧道襯砌體與盾殻之後端部分重合之長度變長。 本發明係藉由提供如下之盾尾間隙測量裝置而達成上述目的者,該盾尾間隙測量裝置係測量被保持於潛盾機之盾殻、與由在該盾殻之後部組裝之環片構成之隧道襯砌體之外周面之間之盾尾間隙的間隙量者,且構成為包含:基台部;旋轉軸部,其以可旋轉地支持於該基台部之狀態設置;旋轉角感測器,其檢測該旋轉軸部之旋轉角;接觸手部,其與上述旋轉軸部接合為一體且朝上述盾殻之後方側延伸設置;及旋轉彈推機構,其以使該接觸手部朝向上述盾殻之中心軸側旋動之方式對上述旋轉軸部賦予旋轉彈推力;且上述旋轉彈推機構具備釋放旋轉彈推力而使上述旋轉軸部朝相反方向旋轉之反轉機構,以使上述接觸手部朝上述盾殻之中心軸之相反側旋動之方式使上述旋轉軸部旋轉,可將上述接觸手部收納於上述基台部之高度範圍。 並且,本發明之盾尾間隙測量裝置較佳為,上述旋轉彈推機構為旋轉致動器。 又,本發明之盾尾間隙測量裝置較佳為,上述旋轉彈推機構為氣壓式旋轉致動器。 進而,本發明之盾尾間隙測量裝置較佳為,上述接觸手部具有於臂本體部之前端具備旋轉輥接觸部之臂形狀。 進而又,本發明之盾尾間隙測量裝置較佳為,設置有使上述基台部之收納上述接觸手部之部分噴出空氣之空氣噴出機構。 又,本發明係藉由提供如下之盾殻而達成上述目的者,該盾殻係安裝有上述盾尾間隙測量裝置者,且於配置有由組裝之環片構成之隧道襯砌體之後端部分,在內周面形成有安裝凹部,將上述盾尾間隙測量裝置以使上述接觸手部朝上述盾殻之軸向後方側延伸,且不使上述基台部自上述盾殻之內周面突出之狀態固定於該安裝凹部。 並且,本發明之盾尾間隙測量裝置較佳為,上述安裝凹部於後部之周向上隔開間隔地設置於至少3個部位,且於各個上述安裝凹部固定有上述盾尾間隙測量裝置。In the above-mentioned previous device or method for measuring the gap of the shield tail, due to durability problems, or because it is difficult to accurately measure the gap amount because the gap amount is not directly measured mechanically, the applicant of this case disclosed in Patent Document 7 that The following shield tail gap measuring device and shield shell: the gap amount of the shield tail gap can be continuously and mechanically measured, the change can be easily grasped, and it has considerable durability that can be placed between the tunnel lining body and the shield shell for a long period of time , And can be easily replaced. However, according to the shield tail gap measuring device or the shield case described in Patent Document 7, the contact hand disposed in a state where the side of the shield case is in contact with the outer peripheral surface of the ring piece uses the spring portion as a spring pushing mechanism for measurement. In the middle, it is always pushed in a rotating manner toward the center axis of the shield shell. Therefore, as shown in FIGS. 9 (a) and (b), if the shield shell 52 is advanced relative to the tunnel lining 51, the shield tail is installed. The part of the gap measuring device 50 exceeds the front end of the assembled tunnel lining body 51, and the contact hand 53 protrudes toward the center axis side of the tunnel lining body 51 from the outer peripheral surface of the tunnel lining body 51 due to the force of the spring portion. It may be a hindrance when assembling the next tunnel lining body 51, or there may be damage due to contact with the hand 53 between the tunnel lining body 51 sandwiched at the front end and the next assembled tunnel lining body 51. Therefore, in the previous method, as shown in FIG. 9 (c), the following research was carried out: by making the shield shell 52 advance and stay to the tunnel lining body where the shield tail gap measuring device 50 is installed does not exceed the assembly At the front end of 51, when assembling the next tunnel lining body 51, the contact hand 53 will not protrude toward the central axis side of the tunnel lining body 51 due to the force of the spring portion; however, the shield shell 52 needs to be correspondingly The length of the rear end of the assembled tunnel lining 51 and the shield shell 52 becomes longer because the construction cannot be performed efficiently. If the length at which the rear end of the assembled tunnel lining body 51 and the shield shell 52 overlap becomes longer, obstacles will occur particularly during the construction of sharply curved curved portions. Therefore, it is desirable to shorten the tunnel lining body and shield shell as much as possible. The rear end part overlaps the length. An object of the present invention is to provide a shield tail gap measuring device and a shield shell, which do not touch the hand even if the shield shell advances relative to the tunnel lining body to a front end of the tunnel lining body assembled with the measuring device. It will protrude toward the center axis side of the tunnel lining body than the outer periphery of the tunnel lining body, which will not become an obstacle when assembling the next tunnel lining body, and can effectively suppress the rear end of the assembled tunnel lining body and shield shell The overlapping length becomes longer. The present invention achieves the above-mentioned object by providing a shield tail gap measuring device which measures a shield case held on a submersible shield machine and is composed of a ring piece assembled at the rear of the shield case The amount of gap between the shield tail gap between the outer surface of the tunnel lining body and the structure includes: abutment portion; a rotating shaft portion which is rotatably supported by the abutment portion; and rotation angle sensing A device that detects the rotation angle of the rotating shaft portion; a contact hand portion that is integrated with the rotating shaft portion and extends toward the rear side of the shield shell; and a rotating spring pushing mechanism that makes the contacting hand portion face The center shaft side of the shield case rotates to impart a rotary elastic thrust to the rotary shaft portion; and the rotary elastic thrust mechanism is provided with a reversing mechanism that releases the rotary elastic thrust and rotates the rotary shaft portion in the opposite direction, so that By rotating the rotating shaft portion by rotating the contact hand toward the opposite side of the central axis of the shield case, the contact hand can be stored in the height range of the base portion. In addition, in the shield tail gap measuring device of the present invention, it is preferable that the rotary elastic pushing mechanism is a rotary actuator. In the shield tail gap measuring device of the present invention, it is preferable that the rotary elastic pushing mechanism is a pneumatic rotary actuator. Furthermore, in the shield tail gap measuring device of the present invention, it is preferable that the contact hand portion has an arm shape including a rotating roller contact portion at a front end of the arm body portion. Furthermore, the shield tail gap measuring device of the present invention is preferably provided with an air ejection mechanism that ejects air from the portion of the base portion that houses the contacting hand portion. In addition, the present invention achieves the above-mentioned object by providing a shield case which is equipped with the above-mentioned shield tail gap measuring device and is provided with a rear end portion of a tunnel lining body composed of an assembled ring piece, A mounting recess is formed on the inner peripheral surface, and the shield tail gap measuring device is extended so that the contact hand portion is axially rearward of the shield case, and the base portion does not protrude from the inner peripheral surface of the shield case. The state is fixed to the mounting recess. In addition, in the shield tail gap measuring device of the present invention, it is preferable that the mounting recesses are provided at least three locations at intervals in the circumferential direction of the rear portion, and the shield tail gap measuring devices are fixed to the mounting recesses.

如圖1~圖3所示,本發明之較佳之一實施形態之盾尾間隙測量裝置10於構成潛盾機11之外廓體之盾殻12之後端部,在周向上隔開間隔地安裝於至少3個部位(於本實施形態中係上下左右4個部位)而使用,且可藉由檢測使以與隧道襯砌體14之外周面接觸方式被彈推之接觸手部19旋動之旋轉軸部17(參照圖2、圖3)之旋轉角,而連續地測量保持於在盾殻12之後部內側組裝環片13而形成之隧道襯砌體14之外周面、與盾殻12之內周面之間的盾尾間隙15之間隙量之變化。本實施形態之盾尾間隙測量裝置10具備輕量且簡易之構成,並且耐久性優異,且可藉由自盾殻12內部之作業而容易更換,故維護性亦優異。藉此,於跨及數月至數年左右之長期限之盾構隧道工程中,即使於長期間持續配置於隧道襯砌體14與盾殻12之間之間隙之情形時,亦能以穩定之狀態連續地測量盾尾間隙15之間隙量。 又,本實施形態之盾尾間隙測量裝置10具備如下功能:藉由使旋轉軸部17旋轉之旋轉彈推機構20(參照圖4、圖5(a)、(b))具備可將接觸手部19之旋轉彈推力釋放而使接觸手部19朝與彈推方向相反方向旋動之反轉機構20a(參照圖6(a)、(b)),即使藉由推進千斤頂35使盾殻12相對於隧道襯砌體14前進至安裝有該測量裝置10之部分超過組裝而成之隧道襯砌體14之前端,接觸手部19亦不會較隧道襯砌體14之外周面朝隧道襯砌體14之中心軸側凸出(參照圖7(b)),故於利用環片13組裝下一個隧道襯砌體14時,凸出之接觸手部19不會成為阻礙(參照圖7(c))。 並且,如圖1~圖3所示,本實施形態之盾尾間隙測量裝置10係測量被保持於潛盾機11之盾殻12、與由在盾殻12之後部組裝之環片13構成之隧道襯砌體14之外周面之間之盾尾間隙15之間隙量的測量裝置,且如圖3~圖5(a)、(b)所示,例如構成為包含:基台部16,其可收納於形成在盾殻12後部之安裝凹部23且具有較佳為小於盾殻12之壁厚之高度;旋轉軸部17,其以可旋轉地支持於基台部16之狀態設置;旋轉角感測器18(參照圖5(a)、(b)),其檢測旋轉軸部17之旋轉角;接觸手部19,其與旋轉軸部17接合為一體且朝盾殻12之後方側延伸設置;及旋轉彈推機構20(參照圖4、圖5(a)、(b)),其以使接觸手部19朝向盾殻12之中心軸側(亦為圖3之上方側、隧道襯砌體14之中心軸側)旋動之方式對旋轉軸部17賦予旋轉彈推力。旋轉彈推機構20具備可釋放旋轉彈推力而使旋轉軸部17朝相反方向旋轉之反轉機構20a(參照圖6(a)、(b)),以接觸手部19朝盾殻12中心軸之相反側(圖3之下方側)旋動之方式使旋轉軸部17旋轉,可將接觸手部19收納於基台部16之高度範圍(參照圖7(b))。 於本實施形態中,潛盾機11為例如泥土壓式之潛盾機,如圖1所示,於壁厚為例如28~50 mm左右(於本實施形態中為50 mm)之圓筒形狀之金屬製外殼體即盾殻12之前端部具備旋轉切割器30,且於盾殻12之內側具備藉由隔板31隔開之泥土壓室32、切割器驅動裝置33、利用螺旋輸送機之排土機構34、推進千斤頂35、環片組裝用之安裝裝置36等。並且,潛盾機11係使用安裝裝置36組裝由環片13構成之隧道襯砌體14,自組裝而成之隧道襯砌體14獲取反作用力,並且利用推進千斤頂35將旋轉切割器30與盾殻12一起推向前方,藉此切削挖掘面,並且一面將切削下之土砂作為泥土經由排土機構34排出,一面鑽掘隧道。 又,於本實施形態中,於使潛盾機11前進時,可在保留組裝而成之隧道襯砌體14的狀態下使盾殻12沿著隧道襯砌體14之外周面順利地向前方移動,並且為了在對曲線部分進行施工時亦能應對,而於組裝成之隧道襯砌體14之外周面、與覆蓋其之盾殻12後部之內周面之間保持盾尾間隙15。於本實施形態中,可藉由利用盾尾間隙測量裝置10連續地測量使潛盾機11前進時之盾尾間隙15之間隙量並掌握其變化,而防止例如於盾殻12之尾部(後端部分),因隧道襯砌體14與盾殻12之干涉導致環片13產生變形或破損,從而可提高隧道襯砌體14之品質。 並且,如圖3~圖5(a)、(b)所示,本實施形態之盾尾間隙測量裝置10構成為包含基台部16、旋轉軸部17、旋轉角感測器18、接觸手部19、及旋轉彈推機構20。於本實施形態中,旋轉彈推機構20較佳為氣壓式旋轉致動器(參照圖6)。 基台部16例如形成為包含底盤部16a與一對軸承壁部16b、16b(參照圖4),且自與盾殻12之中心軸平行之方向觀察時具備コ字剖面形狀,上述底盤部16a具有矩形狀之平面形狀,且大小為配置於與盾殻12之中心軸平行之方向之邊部之長度L1為70 mm左右,配置於與盾殻12之中心軸垂直之方向之邊部之長度L2為40 mm左右(參照圖5(a)),上述一對軸承壁部16b、16b係於中間部分隔開10~15 mm左右之間隔,自底盤部16a之兩側部分立設為一體而設置,且以與盾殻12之中心軸平行地延伸設置之方式配置。基台部16係底盤部16a之下表面至一對軸承壁部16b、16b之上端面之高度h1(參照圖4)為例如30 mm,藉此,基台部16較佳為具有小於例如50 mm盾殻之壁厚之高度。再者,於盾尾間隙測量裝置10之基台部16之高度大於盾殻12之壁厚之情形時,例如可藉由使形成後述之安裝凹部23之底面之鋼製板23a朝盾殻12之外側鼓出設置,使得基台部16不會較盾殻12之內周面更向內側突出。 於基台部16,旋轉軸部17於介存有軸承機構16d(參照圖5(b))等的情況下可旋轉地支持於兩側之軸承壁部16b、16b,且以跨及兩側之軸承壁部16b、16b,於與盾殻12之中心軸垂直之方向上貫通之狀態設置。於コ字剖面形狀之基台部16之一對軸承部16b、16b之間之間隔部分16c,當使後述之接觸手部19朝盾殻12中心軸側之相反側旋動時,收納接觸手部19之臂本體部19a之基端部分(參照圖4)。 旋轉軸部17較佳為金屬製之具有大致圓柱形狀之棒狀構件,如圖5(b)所示,具備直徑增大之中央部分之中央部擴徑部17a、及直徑小於中央部擴徑部17a之兩端部分之一對端部縮徑部17b。於將旋轉軸部17安裝於基台部16時,中央部擴徑部17a配置於一對軸承壁部16b、16b之間之間隔部分16c。兩端部分之端部縮徑部17b分別以於介存有軸承機構16d之情況下可旋轉地被支持之狀態配置於形成在一對軸承壁部16b、16b之插通孔16e。 又,於配置於基台部16之一對軸承壁部16b、16b之間之間隔部分16c之中央部擴徑部17c,形成有於徑向貫通之周面接合孔17c。自接觸手部19之臂本體部19a之一端部一體地突出之接合銷19b以嵌入之方式固定於該周面接合孔17c。藉此,接觸手部19以能夠與旋轉軸部17一起旋轉之方式與旋轉軸部17接合為一體。於配置於形成在一對軸承壁部16b、16b之各個插通孔16e之兩側之端部縮徑部17b,在其等之端面,將端面接合孔17f於旋轉軸部17之軸向上延伸設置。藉由將旋轉角感測器18之感測器軸18a以嵌入之方式固定於一端部縮徑部17b之端面接合孔17f,旋轉角感測器18可測量旋轉軸部17之旋轉角度。藉由將旋轉彈推機構20之接合銷20b以嵌入之方式固定於另一端部縮徑部17b之端面接合孔17f,旋轉軸部17可藉由旋轉彈推機構20之驅動向正方向或反方向旋轉。 進而,於基台部16之一對軸承壁部16b、16b之各者,如圖4所示,於與盾殻12之中心軸平行之方向之兩側端部,形成有於上下方向貫通軸承壁部16b、16b之螺栓緊固固定孔16f。藉由將螺栓構件(未圖示)插通至該等螺栓緊固固定孔16f,並緊固於設置在後述之安裝凹部23之底面部之母螺紋緊固孔,能夠將盾尾間隙測量裝置10可裝卸更換地固定於安裝凹部23。 旋轉角感測器18可使用作為檢測旋轉之物體與不旋轉之物體間之旋轉差量之感測器而公知之例如旋轉編碼器等。於本實施形態中,如圖5(a)、(b)所示,旋轉角感測器18以藉由與基台部16之一軸承壁部16b之外側部分安裝為一體之蓋體21覆蓋,且藉由蓋體21支持並且被防護之狀態設置。旋轉角感測器18可藉由如上所述般將感測器軸18a嵌入至旋轉軸部17之一端部縮徑部17b之端面接合孔17f而測量旋轉軸部17之旋轉角度。 又,於蓋體21將防水連接器21a以朝外部突出之狀態設置。可將沿著盾殻12之內側面延伸設置之感測器纜線22(參照圖2)藉由經由防水連接器21a導入至蓋體21之內部,而連接於旋轉角感測器18。藉此,將由旋轉角感測器18檢測出之角度資訊等信號經由感測器纜線22提取至設置於潛盾機11之內部之例如機內定序器盤。 於本實施形態中,如圖4及圖5(a)、(b)所示,接觸手部19具有於臂本體部19a之前端具備一對旋轉輥接觸部19c之臂形狀。接觸手部19之臂本體部19a例如使用具有12 mm左右之粗度且具有120 mm左右之長度之鋼製桿狀構件而形成,且於一端部具有較臂本體部19a略微縮徑之接合銷19b。如上所述,將接合銷19b嵌入至基台部16之一對軸承壁部16b、16b之間之間隔部分16c中形成於旋轉軸部17之中央部擴徑部17a的周面接合孔17c,且例如經由固定銷一體固定於中央部擴徑部17a,藉此,接觸手部19可伴隨旋轉軸部17之旋轉朝正方向或反方向旋動。 又,於臂本體部19a之與接合銷19b為相反側之另一端部,形成有將兩側之側面平行地進行倒角之缺口面19d,並以貫通兩側之缺口面19d之方式將旋轉支持軸19e以朝兩側突出之狀態設置。一對旋轉輥接觸部19c經由軸承機構等可旋轉地支持於自缺口面19d朝兩側突出之部分之旋轉支持軸19e,且設置於隔著臂本體部19a之另一端部之兩側。 旋轉輥接觸部19c使用具備較臂本體部19a之外徑更大之外徑之例如20 mm左右之粗度之鋼製套筒構件而形成。旋轉輥接觸部19c藉由在介存有由多個球體構成之軸承機構的情況下安裝於朝缺口面19d之兩側突出之部分之旋轉支持軸19e,而能以旋轉支持軸19e為旋轉中心旋轉地安裝。旋轉輥接觸部19c於藉由對接觸手部19彈推之旋轉彈推機構20之作用力旋動而接觸於由環片13構成之隧道襯砌體14之外周面時能夠旋轉,故能以更順利且穩定之狀態使接觸手部19沿著隧道襯砌體14之外周面朝盾殻12之軸向移動。 於本實施形態中,如上所述,旋轉彈推機構20較佳為使用例如氣壓式旋轉致動器作為旋轉致動器。旋轉致動器係作為可調節搖動角度之裝置而公知者,亦可使用例如油壓式旋轉致動器或電動式旋轉致動器。氣壓式旋轉致動器係以氣壓為驅動源之致動器,例如作為單葉片類型者具備如圖6(a)、(b)所示之構造。圖6(a)、(b)所示之氣壓式旋轉致動器之彈推機構20構成為包含:本體40;葉片41,其於本體40之內表面滑動;旋轉軸42,其與葉片41成一體;擋止件43;及反轉機構20a,其包含成為空氣供給口之A埠及B埠,如圖6(a)所示,當自A埠供給空氣時,葉片41被按壓而對旋轉軸42產生轉矩,並且排氣側室之空氣通過B埠被排出,且例如可於葉片41碰撞到擋止件43而停止之前繞順時針方向旋轉。又,當自B埠供給空氣時,如圖6(b)所示,可同樣地繞逆時針方向旋轉。 因此,於本實施形態中,於連續測量保持於組裝環片13形成之隧道襯砌體14之外周面、與盾殻12之內周面之間的盾尾間隙15之間隙量之變化時,例如自A埠供給空氣使旋轉軸42產生轉矩,藉此可經由與旋轉軸42連結之接合銷20b對旋轉軸部17賦予旋轉彈推力,以使接觸手部19朝盾殻12之中心軸側旋動(參照圖3、圖7(a))。又,於使盾殻12相對於隧道襯砌體14前進至安裝有測量裝置10之部分超過組裝而成之隧道襯砌體14之前端時,例如藉由自B埠供給空氣使反轉機構20a作動,釋放經由旋轉軸42及接合銷20b之旋轉軸部17之旋轉彈推力,進而以使接觸手部19朝向盾殻12中心軸之相反側旋動之方式使旋轉軸部17旋轉,藉此可將接觸手部19收納於基台部16之高度範圍(參照圖7(b)、(c))內。 又,於本實施形態中,於作為旋轉彈推機構20之氣壓式旋轉致動器,以自外周面向外側突出之方式突出地設置有一對配管埠20c(參照圖4)。各個配管埠20c與用以將空氣供給至氣壓式旋轉致動器20之本體40內部之A埠及B埠連續。可藉由於各個配管埠20c連接沿著盾殻12之內側面延伸設置之空氣供給配管24(參照圖5(a)),一面切換成為空氣供給口之A埠及B埠,一面將空氣壓送供給至本體40之內部。 進而,於本實施形態中,如圖8所示,於基台部16之收納接觸手部19之部分即コ字剖面形狀之基台部16之一對軸承壁部16b、16b之間之間隔部分16c,於底盤部16a之上表面開口且使該底盤部16a之上表面噴出空氣之空氣噴出孔25作為空氣噴出機構以與空氣供給套筒26(參照圖4)連通之狀態設置。藉由自該空氣噴出孔25較佳為始終連續地噴出自空氣供給套筒26送入之空氣,可避免土砂或回填材堆積於收納接觸手部19之部分,或異物侵入。藉此,可有效地避免於使接觸手部19朝盾殻12中心軸側之相反側旋動時,難以將接觸手部19之臂本體部19a之基端部分收容於間隔部分16c,而無法將接觸手部19收納於基台部16之高度範圍。 於本實施形態中,具備上述構成之盾尾間隙測量裝置10係以各種固定之狀態安裝於安裝凹部23而使用(參照圖1~圖3),上述安裝凹部23於盾殻12之配置有由組裝之環片13構成之隧道襯砌體14之後部,例如於周向上以90度之等角度間隔設置於上下左右4個部位。 即,於本實施形態中,如圖2及圖3所示,於盾殻12之後部,能夠收納盾尾間隙測量裝置10整體之大小之安裝凹部23藉由將鋼製板23a熔接而閉塞例如形成於盾殻12之貫通開口之外周面側部分,而形成於上下左右之4個部位。將盾尾間隙測量裝置10以使接觸手部19朝盾殻12之軸向後方側延伸設置之狀態,且以使一體安裝有蓋體21或旋轉彈推機構20之基台部16不自盾殻12之內周面突出之狀態固定於該等安裝凹部23。盾尾間隙測量裝置10例如可藉由朝向成為安裝凹部23之底面之鋼製板23a之特定位置所形成之母螺紋緊固孔,將螺栓構件(未圖示)插通並緊固於貫通形成於基台部16之一對軸承壁部16b、16b各者之螺栓緊固固定孔16f,而可裝卸更換地容易地固定於安裝凹部23。 又,於本實施形態中,於盾殻12之內側面,切開形成有分別自4個部位之安裝凹部23朝盾殻12之軸向前方側延伸設置,且用以供配設感測器纜線22或空氣供給配管24等之凹槽27。藉由於該凹槽27敷設感測器纜線22而將設置於安裝凹部23之盾尾間隙測量裝置10之旋轉角感測器18、與設置於潛盾機11內部之例如機內定序器盤連接。又,藉由於該凹槽27敷設空氣供給配管24等而可將例如自壓縮機輸送之壓縮空氣供給至空氣壓縮式旋轉致動器之旋轉彈推機構20,或經由空氣供給套筒26自空氣噴出孔25噴出。 如上所述般固定於安裝凹部23之盾尾間隙測量裝置10於盾殻12之後部內側組裝由環片13構成之隧道襯砌體14後,如圖2及圖3所示,保持利用氣壓式轉送裝置之旋轉彈推機構20之作用力將接觸手部19之旋轉輥接觸部19c始終自盾殻12之後方側接觸於隧道襯砌體14之外周面之狀態,因而可藉由旋轉角感測器18容易地檢測出因盾尾間隙之間隙量之變化所致之接合有接觸手部19之旋轉軸部17之旋轉角的變化。又,固定於安裝凹部23之盾尾間隙測量裝置10可連續測量盾尾間隙15之間隙量,並容易地掌握其變化,並且具備可長期間地配置於隧道襯砌體14與盾殻12之間之相當之耐久性,且亦可容易地進行更換作業。 並且,根據具備上述構成之本實施形態之盾尾間隙測量裝置10及盾殻12,即使盾殻12相對於隧道襯砌體14前進至安裝有測量裝置10之部分超過組裝而成之隧道襯砌體14之前端,接觸手部19亦不會較隧道襯砌體14之外周面朝盾殻12之中心軸側凸出,不會成為組裝下一個隧道襯砌體14時之阻礙,且可有效地抑制組裝而成之隧道襯砌體14與盾殻12之後端部分重合之長度變長。 即,根據本實施形態,盾尾間隙測量裝置10構成為包含:基台部16,其具有小於盾殻12之壁厚之高度;旋轉軸部17,其以可旋轉地支持於基台部16之狀態設置;旋轉角感測器18,其檢測旋轉軸部17之旋轉角;接觸手部19,其與旋轉軸部17接合為一體且朝盾殻12之後方側延伸設置;及旋轉彈推機構20,其以使接觸手部19朝向盾殻12之中心軸側旋動之方式對旋轉軸部17賦予旋轉彈推力;旋轉彈推機構20具備可釋放旋轉彈推力而使旋轉軸部17朝相反方向旋轉之反轉機構20a,以接觸手部19朝向盾殻12中心軸之相反側旋動之方式使旋轉軸部17旋轉,可將接觸手部19收納於基台部16之高度範圍。 因此,於本實施形態中,於盾殻12之後部內側組裝由環片13構成之隧道襯砌體14後,如圖7(a)所示,保持利用旋轉彈推機構20之作用力將接觸手部19之旋轉輥接觸部19c始終自盾殻12之後方側接觸於隧道襯砌體14之外周面之狀態,因而可容易地檢測出因盾尾間隙15之間隙量之變化所致之接合有接觸手部19之旋轉軸部17之旋轉角的變化,藉此,可容易地連續測量盾尾間隙之間隙量之變化。 又,於使推進千斤頂35伸長而使盾殻12相對於隧道襯砌體14前進時,如圖7(b)所示,例如於推進千斤頂35完全伸長之前,以反轉機構20a較佳為自動地將空氣供給口自A埠切換為B埠之方式,與推進千斤頂35之伸長狀況連動地控制旋轉彈推機構20(參照圖6(a)、(b))。藉此,於安裝有測量裝置10之部分超過組裝而成之隧道襯砌體14之前端之前,旋轉彈推機構20釋放旋轉彈推力,並且以接觸手部19朝向盾殻12中心軸之相反側旋動之方式使旋轉軸部17旋轉,可將接觸手部19收納於基台部16之高度範圍。 又,藉此,如圖7(c)所示,即使於推進千斤頂35完全伸長使得盾殻12相對於隧道襯砌體14前進至安裝有測量裝置10之部分超過組裝而成之隧道襯砌體14之前端,亦可實現接觸手部19不較隧道襯砌體14之外周面朝盾殻12之中心軸側凸出,不會成為藉由環片13組裝下一個隧道襯砌體14時之阻礙,且可有效地抑制組裝而成之隧道襯砌體14與盾殻12之後端部分重合之長度變長。 進而,於利用環片13組裝下一個隧道襯砌體14時之作業中,中斷旋轉軸部17之旋轉角之檢測,且於下一個隧道襯砌體14組裝結束後,按下例如控制裝置之測量準備完成按鈕,藉此將空氣供給口切換為A埠,如圖7(d)所示,使接觸手部19之旋轉輥接觸部19c自盾殻12之後方側接觸於隧道襯砌體14之外周面,重新開始旋轉軸部17之旋轉角之檢測,且使推進千斤頂35伸長,重新開始潛盾機11之鑽掘作業。 再者,本發明不限定於上述實施形態而可有各種變更。例如,旋轉彈推機構未必為氣壓式旋轉致動器等旋轉致動器,亦可使用具備釋放旋轉彈推力使旋轉軸部朝相反方向旋轉之反轉機構之其他公知之各種旋轉彈推機構。又,接觸手部未必具有於本體部之前端具備旋轉輥接觸部之臂形狀,亦可使用其他各種接觸手部。進而,未必設置使基台部之收納接觸手部之部分噴出空氣之空氣噴出機構。例如,亦可於基台部之收納接觸手部之部分、與接觸手部之間設置膜機構,而不會使土砂或回填材堆積、或異物侵入。 [產業上之可利用性] 根據本發明之盾尾間隙測量裝置或盾殻,即使盾殻相對於隧道襯砌體前進至安裝有測量裝置之部分超過組裝而成之隧道襯砌體之前端,接觸手部亦不會較隧道襯砌體之外周面朝隧道襯砌體之中心軸側凸出,不會成為組裝下一個隧道襯砌體時之阻礙,且可有效地抑制組裝而成之隧道襯砌體與盾殻之後端部分重合之長度變長。As shown in FIG. 1 to FIG. 3, a shield tail gap measuring device 10 according to a preferred embodiment of the present invention is installed behind the shield shell 12 constituting the outer body of the submersible shield 11 at intervals in the circumferential direction. It is used in at least 3 places (in this embodiment, up, down, left, and right 4 places), and can be rotated by contact with the contact hand 19 that is pushed by the contact with the outer peripheral surface of the tunnel lining body 14 by detection The rotation angle of the shaft portion 17 (see FIGS. 2 and 3) is continuously measured and maintained on the outer peripheral surface of the tunnel lining body 14 formed by assembling the ring piece 13 on the inner side of the rear portion of the shield case 12 and the inner periphery of the shield case 12. Changes in the amount of the gap between the shield tail gaps 15 between the faces. The shield tail gap measuring device 10 of this embodiment has a lightweight and simple structure, is excellent in durability, and can be easily replaced by operations from the inside of the shield shell 12, so it is also excellent in maintainability. In this way, in the long-term shield tunnel project spanning several months to several years, even when the gap between the tunnel lining body 14 and the shield shell 12 is continuously arranged for a long period of time, it can be stabilized. The gap amount of the shield tail gap 15 is continuously measured. In addition, the shield tail gap measuring device 10 of this embodiment has a function of providing a contact hand by a rotary spring pushing mechanism 20 (see FIGS. 4 and 5 (a) and (b)) that rotates the rotating shaft portion 17. The reversing mechanism 20 a (see FIGS. 6 (a) and (b)) of the rotating projectile force of the rotary projectile 19 which releases the contact hand 19 in a direction opposite to the projectile pushing direction, even if the shield case 12 is pushed by pushing the jack 35. With respect to the tunnel lining body 14, the portion where the measuring device 10 is installed exceeds the front end of the assembled tunnel lining body 14, and the contact hand 19 will not face the center of the tunnel lining body 14 from the outer periphery of the tunnel lining body 14. The shaft side protrudes (see FIG. 7 (b)). Therefore, when the next tunnel lining body 14 is assembled using the ring piece 13, the protruding hand 19 does not become an obstacle (see FIG. 7 (c)). Further, as shown in FIGS. 1 to 3, the shield tail gap measuring device 10 of this embodiment measures the shield case 12 held by the submersible shield 11 and the ring piece 13 assembled at the rear of the shield case 12. The device for measuring the gap amount of the shield tail gap 15 between the outer peripheral surface of the tunnel lining body 14 and, as shown in FIGS. 3 to 5 (a) and (b), includes, for example, an abutment portion 16 which can It is housed in a mounting recess 23 formed at the rear of the shield case 12 and preferably has a height smaller than the wall thickness of the shield case 12; a rotating shaft portion 17 is rotatably supported by the base portion 16; Detector 18 (refer to FIGS. 5 (a) and (b)), which detects the rotation angle of the rotating shaft portion 17; contacting the hand portion 19, which is integrated with the rotating shaft portion 17 and extends toward the rear side of the shield case 12 ; And a rotary ejection mechanism 20 (see FIGS. 4 and 5 (a) and (b)), so that the contact hand 19 faces the central axis side of the shield shell 12 (also the upper side of FIG. 3, the tunnel lining body); The center axis side of 14) rotates to impart a rotating elastic thrust to the rotating shaft portion 17. The rotary spring pushing mechanism 20 is provided with a reversing mechanism 20a (see FIGS. 6 (a) and (b)) that can release the rotary spring pushing force and rotate the rotary shaft portion 17 in the opposite direction, and contacts the hand 19 toward the center axis of the shield case 12. On the opposite side (lower side in FIG. 3), the rotating shaft portion 17 is rotated, and the contact hand portion 19 can be stored in the height range of the base portion 16 (see FIG. 7 (b)). In this embodiment, the submersible shield machine 11 is, for example, a soil pressure type submersible shield machine. As shown in FIG. 1, the submersible shield machine 11 has a cylindrical shape with a wall thickness of, for example, about 28 to 50 mm (in this embodiment, 50 mm). The metal outer casing, that is, the front end of the shield shell 12, is provided with a rotary cutter 30, and inside the shield shell 12 is provided with a soil pressure chamber 32 separated by a partition plate 31, a cutter driving device 33, and a screw conveyor. The soil discharging mechanism 34, the pushing jack 35, the mounting device 36 for ring plate assembly, and the like. In addition, the submersible shield 11 uses the mounting device 36 to assemble the tunnel lining body 14 composed of the ring sheet 13. The self-assembled tunnel lining body 14 obtains a reaction force, and uses a pushing jack 35 to connect the rotary cutter 30 and the shield shell 12. Push forward together to cut the digging surface, and excavate the cut soil and sand as dirt through the discharge mechanism 34, while digging the tunnel. Further, in this embodiment, when the submersible shield 11 is advanced, the shield shell 12 can be smoothly moved forward along the outer peripheral surface of the tunnel lining body 14 while the assembled tunnel lining body 14 is retained. In addition, in order to cope with the construction of the curved portion, a shield tail gap 15 is maintained between the outer peripheral surface of the assembled tunnel lining body 14 and the inner peripheral surface of the rear portion of the shield shell 12 covering it. In this embodiment, by using the shield tail gap measuring device 10 to continuously measure the gap amount of the shield tail gap 15 when the submersible shield 11 is advanced and grasp the change, it is possible to prevent, for example, the tail portion of the shield shell 12 (rear End part), the ring lining 13 is deformed or broken due to the interference between the tunnel lining body 14 and the shield shell 12, thereby improving the quality of the tunnel lining body 14. In addition, as shown in FIGS. 3 to 5 (a) and (b), the shield tail gap measuring device 10 of this embodiment is configured to include a base portion 16, a rotating shaft portion 17, a rotation angle sensor 18, and a contact hand.部 19 , Rotary ejection mechanism 20. In this embodiment, the rotary push mechanism 20 is preferably a pneumatic rotary actuator (see FIG. 6). The base portion 16 includes, for example, a chassis portion 16 a and a pair of bearing wall portions 16 b and 16 b (see FIG. 4), and has a U-shaped cross-sectional shape when viewed from a direction parallel to the central axis of the shield case 12. It has a rectangular planar shape and has a length L1 arranged at a side parallel to the center axis of the shield shell 12 of about 70 mm and a length arranged at a side perpendicular to the center axis of the shield shell 12 L2 is about 40 mm (refer to FIG. 5 (a)). The pair of bearing wall portions 16b and 16b are spaced at an interval of about 10 to 15 mm at the middle portion, and are integrally formed from both sides of the chassis portion 16a. It is arranged, and it is arrange | positioned so that it may extend and arrange in parallel with the center axis of the shield case 12. The height h1 (see FIG. 4) of the base portion 16 from the lower surface of the chassis portion 16 a to the upper end surfaces of the pair of bearing wall portions 16 b and 16 b is, for example, 30 mm. Therefore, the base portion 16 preferably has a height of less than 50, for example. mm The height of the wall thickness of the shield shell. Furthermore, when the height of the base portion 16 of the shield tail gap measuring device 10 is greater than the wall thickness of the shield case 12, for example, the steel plate 23a forming the bottom surface of the mounting recess 23 described later may be directed toward the shield case 12. The outer side is bulged so that the abutment portion 16 does not protrude more inward than the inner peripheral surface of the shield shell 12. The base portion 16 and the rotating shaft portion 17 are rotatably supported on the bearing wall portions 16b and 16b on both sides when a bearing mechanism 16d (see FIG. 5 (b)) is interposed therebetween, and are arranged across the both sides. The bearing wall portions 16 b and 16 b are provided in a state penetrating in a direction perpendicular to the central axis of the shield case 12. The space 16c between the pair of bearing portions 16b and 16b of one of the base portions 16 in the U-shaped cross-section is accommodated when the contact hand 19 described later is rotated toward the opposite side of the center axis side of the shield case 12. The base end portion of the arm body portion 19a of the portion 19 (see FIG. 4). The rotating shaft portion 17 is preferably a metal rod-shaped member having a substantially cylindrical shape. As shown in FIG. 5 (b), the rotating shaft portion 17 includes a central portion enlarged portion 17a having a central portion with an increased diameter, and a diameter smaller than that of the central portion. One of both end portions of the portion 17a is a pair of end reduced-diameter portions 17b. When the rotation shaft portion 17 is mounted on the base portion 16, the central portion enlarged diameter portion 17 a is disposed at the space portion 16 c between the pair of bearing wall portions 16 b and 16 b. The reduced-diameter end portions 17b of the both end portions are respectively disposed in the insertion holes 16e formed in the pair of bearing wall portions 16b and 16b in a state where the bearing mechanism 16d is rotatably supported. In addition, in the central portion enlarged diameter portion 17c of the space portion 16c disposed between the pair of bearing wall portions 16b, 16b of the base portion 16, a circumferential surface engaging hole 17c is formed so as to penetrate in the radial direction. An engaging pin 19b that protrudes integrally from one end of the arm body portion 19a of the contact hand 19 is fixed to the peripheral surface engaging hole 17c by being fitted. Thereby, the contact hand part 19 is integrally joined with the rotating shaft part 17 so that it can rotate together with the rotating shaft part 17. In the reduced diameter portions 17b disposed on both sides of each of the insertion holes 16e formed in the pair of bearing wall portions 16b and 16b, the end surface engaging holes 17f are extended in the axial direction of the rotating shaft portion 17 Settings. The rotation angle sensor 18 can measure the rotation angle of the rotation shaft portion 17 by fixing the sensor shaft 18a of the rotation angle sensor 18 to the end-face engaging hole 17f of the one-end reduced-diameter portion 17b in an embedded manner. By fixing the engaging pin 20b of the rotary ejection mechanism 20 to the end-face engaging hole 17f of the reduced-diameter portion 17b at the other end, the rotary shaft portion 17 can be driven in the forward or reverse direction by the drive of the rotary ejection mechanism 20. Direction rotation. Further, as shown in FIG. 4, each of the pair of bearing wall portions 16 b and 16 b of the base portion 16 is formed with a bearing penetrating in the vertical direction at both end portions in a direction parallel to the central axis of the shield case 12. The wall portions 16b and 16b are fastened with bolts 16f. The shield tail clearance measuring device can be inserted by inserting a bolt member (not shown) into these bolt-fixing fixing holes 16f and tightening the female screw-fastening holes provided in the bottom surface of the mounting recess 23 described later. 10 is detachably fixed to the mounting recess 23. The rotation angle sensor 18 may be a sensor that detects a difference in rotation between a rotating object and a non-rotating object, such as a rotary encoder. In this embodiment, as shown in FIGS. 5 (a) and 5 (b), the rotation angle sensor 18 is covered with a cover body 21 that is integrally mounted with the outer side portion of one of the bearing wall portions 16 b of the base portion 16. And is set by the cover 21 being supported and protected. The rotation angle sensor 18 can measure the rotation angle of the rotation shaft portion 17 by fitting the sensor shaft 18 a into the end-face engaging hole 17 f of the one-end reduced-diameter portion 17 b of the rotation shaft portion 17 as described above. The waterproof connector 21a is provided on the cover body 21 so as to protrude outward. The sensor cable 22 (refer to FIG. 2) extending along the inner side surface of the shield case 12 may be connected to the rotation angle sensor 18 by being introduced into the cover 21 through the waterproof connector 21 a. Thereby, signals such as angle information detected by the rotation angle sensor 18 are extracted via the sensor cable 22 to, for example, an on-board sequencer disk provided inside the submersible shield 11. In this embodiment, as shown in FIGS. 4 and 5 (a) and (b), the contact hand portion 19 has an arm shape including a pair of rotating roller contact portions 19c at the front end of the arm body portion 19a. The arm body portion 19a of the hand 19 is, for example, It is formed by a steel rod-shaped member having a thickness of about 12 mm and a length of about 120 mm, and has an engaging pin 19b at one end portion that is slightly reduced in diameter than the arm body portion 19a. As described above, the engaging pin 19b is fitted into the peripheral surface engaging hole 17c formed in the space portion 16c between the pair of bearing wall portions 16b, 16b of the base portion 16 formed in the central portion enlarged diameter portion 17a of the rotating shaft portion 17, And, for example, it is integrally fixed to the enlarged diameter portion 17a of the central portion via a fixing pin, whereby the contact hand portion 19 can be rotated in the forward or reverse direction along with the rotation of the rotation shaft portion 17. A notch surface 19d is formed at the other end of the arm body portion 19a on the opposite side to the engaging pin 19b. The notch surface 19d is chamfered in parallel on both sides, and is rotated to penetrate the notch surfaces 19d on both sides. The support shaft 19e is provided in a state protruding toward both sides. A pair of rotating roller contact portions 19c are rotatably supported on a rotation supporting shaft 19e of a portion protruding from both sides of the notch surface 19d via a bearing mechanism or the like, and are provided on both sides of the other end portion across the arm body portion 19a. As the rotating roller contact portion 19c, for example, an outer diameter larger than the outer diameter of the arm body portion 19a is used. It is formed by a steel sleeve member with a thickness of about 20 mm. The rotation roller contact portion 19c can be rotated by the rotation support shaft 19e by mounting the rotation support shaft 19e on a portion protruding toward both sides of the notch surface 19d with a bearing mechanism composed of a plurality of balls. Rotate it. The rotating roller contact portion 19c can rotate when contacted with the outer peripheral surface of the tunnel lining body 14 constituted by the ring piece 13 due to the rotating force of the rotating elastic pushing mechanism 20 which is pushed by the contacting hand portion 19, so that the rotating roller contact portion 19c can be rotated even more. The smooth and stable state causes the contact hand 19 to move along the outer peripheral surface of the tunnel lining body 14 toward the axial direction of the shield shell 12. In the present embodiment, as described above, it is preferable that the rotary push mechanism 20 uses, for example, a pneumatic rotary actuator as the rotary actuator. The rotary actuator is known as a device capable of adjusting the swing angle. For example, a hydraulic rotary actuator or an electric rotary actuator may be used. The pneumatic rotary actuator is an actuator that uses air pressure as a driving source. For example, a single-blade type actuator has a structure as shown in FIGS. 6 (a) and (b). The ejection mechanism 20 of the pneumatic rotary actuator shown in Figs. 6 (a) and (b) is composed of: a body 40; a blade 41 which slides on the inner surface of the body 40; a rotation shaft 42 which is connected with the blade 41 Integrated; stopper 43; and reversing mechanism 20a, including port A and port B serving as air supply ports, as shown in FIG. 6 (a), when air is supplied from port A, the blade 41 is pressed against The rotating shaft 42 generates a torque, and the air in the exhaust side chamber is exhausted through the B port, and can rotate in a clockwise direction before the blade 41 hits the stopper 43 and stops, for example. When the air is supplied from the B port, as shown in FIG. 6 (b), it can be similarly rotated in the counterclockwise direction. Therefore, in this embodiment, when the change in the gap amount of the shield tail gap 15 between the outer peripheral surface of the tunnel lining body 14 formed by the assembly ring piece 13 and the inner peripheral surface of the shield case 12 is continuously measured, for example, Air is supplied from the A port to generate torque on the rotating shaft 42, so that a rotating elastic thrust can be given to the rotating shaft portion 17 through the joint pin 20 b connected to the rotating shaft 42, so that the contact hand portion 19 faces the center axis side of the shield case 12. Rotate (see Figure 3 and Figure 7 (a)). When the shield shell 12 is advanced relative to the tunnel lining body 14 to the front end of the assembled tunnel lining body 14 where the measuring device 10 is installed, for example, the reversing mechanism 20a is activated by supplying air from the B port, By releasing the thrust force of the rotating spring via the rotating shaft 42 and the rotating shaft portion 17 of the engaging pin 20b, the rotating shaft portion 17 is rotated so that the contact hand portion 19 is rotated toward the opposite side of the center axis of the shield case 12, thereby enabling the rotating shaft portion 17 to be rotated. The contact hand part 19 is accommodated in the height range of the base part 16 (refer FIG.7 (b), (c)). Moreover, in this embodiment, a pair of piping ports 20c are provided so as to protrude so that it may protrude from an outer peripheral surface to the pneumatic rotary actuator which is the rotary ejection mechanism 20 (refer FIG. 4). Each of the piping ports 20c is continuous with the A port and the B port inside the body 40 for supplying air to the pneumatic rotary actuator 20. Since each of the piping ports 20c is connected to the air supply piping 24 (refer to FIG. 5 (a)) extending along the inner side of the shield case 12, the ports A and B can be switched to the air supply port, and the air can be pressure-fed. It is supplied to the inside of the body 40. Further, in this embodiment, as shown in FIG. 8, the space between the pair of bearing wall portions 16 b and 16 b of the base portion 16 which is a portion of the U-shaped cross section of the base portion 16 that is in contact with the hand portion 19 is received. The portion 16c is provided on the upper surface of the chassis portion 16a, and an air ejection hole 25 for ejecting air from the upper surface of the chassis portion 16a is provided as an air ejection mechanism in a state communicating with the air supply sleeve 26 (see FIG. 4). The air sent from the air supply sleeve 26 is preferably continuously ejected from the air ejection hole 25 at all times, so that it is possible to prevent the accumulation of dirt, sand, or backfill material on the part that receives the contact with the hand 19, or the invasion of foreign matter. This can effectively prevent the base end portion of the arm body portion 19a of the contact hand portion 19 from being held in the spacer portion 16c when the contact hand portion 19 is rotated toward the opposite side of the center axis side of the shield case 12, and cannot be prevented. The contact hand portion 19 is stored in the height range of the base portion 16. In this embodiment, the shield tail gap measuring device 10 having the above-mentioned structure is used by being mounted on the mounting recess 23 in various fixed states (refer to FIGS. 1 to 3). The rear portion of the tunnel lining body 14 composed of the assembled ring pieces 13 is provided at four positions, for example, up, down, left, and right, at equal angular intervals of 90 degrees in the circumferential direction. That is, in this embodiment, as shown in FIG. 2 and FIG. 3, at the rear portion of the shield case 12, the mounting recess 23 that can accommodate the entire shield tail gap measuring device 10 can be closed by welding the steel plate 23 a. It is formed in the peripheral surface side part outside the through-opening of the shield case 12, and it is formed in four places of upper, lower, left, and right. The shield tail gap measuring device 10 is provided in a state where the contact hand 19 is extended toward the axially rear side of the shield case 12, and the base portion 16 on which the cover body 21 or the rotary push mechanism 20 is integrally mounted is not removed from the shield case. A state in which the inner peripheral surface of 12 protrudes is fixed to the mounting recesses 23. The shield tail gap measuring device 10 can be formed by, for example, inserting and fastening a bolt member (not shown) through a female screw fastening hole formed at a specific position of the steel plate 23 a that becomes the bottom surface of the mounting recess 23. Bolts are fastened to the bearing wall portions 16 b and 16 b of one of the base portions 16 and fixed to the mounting recesses 23 so that they can be detached and replaced. Moreover, in this embodiment, the inner side surface of the shield case 12 is cut and formed to extend from the mounting recesses 23 at four locations toward the axially forward side of the shield case 12, respectively, and is used to arrange a sensor cable. The grooves 27 of the wire 22 or the air supply pipe 24 and the like. As the sensor cable 22 is laid in the groove 27, the rotation angle sensor 18 of the shield tail gap measuring device 10 installed in the mounting recess 23 and the internal sequencer disk provided inside the shield machine 11 are installed, for example. connection. The air supply piping 24 or the like is laid in the groove 27, so that, for example, compressed air delivered from the compressor can be supplied to the rotary spring mechanism 20 of the air compression rotary actuator, or air can be supplied from the air through the air supply sleeve 26. The ejection hole 25 ejects. As described above, the shield tail gap measuring device 10 fixed to the mounting recess 23 is assembled with a tunnel lining body 14 composed of a ring sheet 13 on the inside of the rear portion of the shield shell 12 as shown in FIGS. 2 and 3. The force of the rotating spring pushing mechanism 20 of the device will be in a state where the rotating roller contact portion 19c contacting the hand portion 19 is always in contact with the outer peripheral surface of the tunnel lining body 14 from the rear side of the shield case 12, so the rotation angle sensor can be used. 18 makes it easy to detect a change in the rotation angle of the rotating shaft portion 17 to which the hand 19 is engaged due to a change in the gap amount of the shield tail gap. In addition, the shield tail gap measuring device 10 fixed to the mounting recess 23 can continuously measure the gap amount of the shield tail gap 15 and easily grasp the change, and is provided between the tunnel lining body 14 and the shield shell 12 for a long period of time. It is quite durable and can be easily replaced. In addition, according to the shield tail gap measuring device 10 and the shield shell 12 of the present embodiment having the above configuration, even if the shield shell 12 advances relative to the tunnel lining body 14 to a portion where the measuring device 10 is installed exceeds the assembled tunnel lining body 14 At the front end, the contact hand 19 will not protrude toward the central axis side of the shield shell 12 from the outer peripheral surface of the tunnel lining body 14, which will not become an obstacle when assembling the next tunnel lining body 14, and can effectively inhibit assembly. The length of the overlapping portion of the tunnel lining body 14 and the rear end of the shield shell 12 becomes longer. That is, according to this embodiment, the shield tail gap measuring device 10 is configured to include: a base portion 16 having a height smaller than the wall thickness of the shield case 12; and a rotating shaft portion 17 which is rotatably supported by the base portion 16. The state setting; a rotation angle sensor 18 that detects the rotation angle of the rotation shaft portion 17; a contact hand portion 19 that is integrated with the rotation shaft portion 17 and extends toward the rear side of the shield case 12; and a rotary spring push A mechanism 20 that imparts a rotary spring thrust to the rotary shaft portion 17 so that the contact hand 19 rotates toward the center axis side of the shield case 12; the rotary spring push mechanism 20 is provided with a rotary spring thrust 17 that can release the rotary spring thrust The reversing mechanism 20 a rotating in the opposite direction rotates the rotating shaft portion 17 so that the contacting hand portion 19 rotates toward the opposite side of the center axis of the shield case 12, and the contacting hand portion 19 can be stored in the height range of the base portion 16. Therefore, in this embodiment, after assembling the tunnel lining body 14 composed of the ring sheet 13 on the inner side of the rear portion of the shield case 12, as shown in FIG. 7 (a), the contact force is maintained by the force of the rotary spring pushing mechanism 20 The rotating roller contact portion 19c of the portion 19 is always in contact with the outer peripheral surface of the tunnel lining body 14 from the rear side of the shield shell 12, so it is easy to detect the contact caused by the change in the gap amount of the shield tail gap 15 By changing the rotation angle of the rotating shaft portion 17 of the hand portion 19, it is possible to easily continuously measure the change in the gap amount of the shield tail gap. Further, when the pushing jack 35 is extended to advance the shield shell 12 relative to the tunnel lining body 14, as shown in FIG. 7 (b), for example, before the pushing jack 35 is fully extended, the reversing mechanism 20a is preferably automatically The method of switching the air supply port from the A port to the B port controls the rotary ejection mechanism 20 in conjunction with the elongation of the propulsion jack 35 (see FIGS. 6 (a), (b)). By this, before the part on which the measuring device 10 is installed exceeds the front end of the assembled tunnel lining body 14, the rotary spring pushing mechanism 20 releases the rotary spring thrust and rotates with the contact hand 19 toward the opposite side of the center axis of the shield shell 12. When the rotating shaft portion 17 is rotated, the contact hand portion 19 can be stored in the height range of the base portion 16. Furthermore, as shown in FIG. 7 (c), even if the pushing jack 35 is fully extended, the shield shell 12 advances relative to the tunnel lining body 14 to a portion where the measuring device 10 is installed exceeds the assembled tunnel lining body 14. At the front end, it can also be achieved that the contact with the hand 19 does not protrude toward the central axis side of the shield shell 12 from the outer peripheral surface of the tunnel lining body 14, and does not become an obstacle when assembling the next tunnel lining body 14 through the ring sheet 13. The length of the overlap of the assembled tunnel lining body 14 and the rear end portion of the shield shell 12 is effectively suppressed. Furthermore, during the operation of assembling the next tunnel lining body 14 using the ring sheet 13, the detection of the rotation angle of the rotating shaft portion 17 is interrupted, and after the assembly of the next tunnel lining body 14 is completed, for example, the measurement preparation of the control device is pressed. Complete the button to switch the air supply port to port A. As shown in Fig. 7 (d), the rotating roller contact portion 19c of the contact hand 19 contacts the outer peripheral surface of the tunnel lining body 14 from the rear side of the shield shell 12 , The detection of the rotation angle of the rotating shaft portion 17 is restarted, the propulsion jack 35 is extended, and the drilling operation of the submersible shield machine 11 is restarted. It should be noted that the present invention is not limited to the above-mentioned embodiment and can be modified in various ways. For example, the rotary push mechanism is not necessarily a rotary actuator such as a pneumatic rotary actuator, and other known rotary push mechanisms including a reversing mechanism that releases the rotary push force and rotates the rotary shaft portion in the opposite direction may be used. In addition, the contact hand does not necessarily have the shape of an arm having a rotating roller contact portion at the front end of the main body portion, and various other contact hands may be used. Furthermore, it is not always necessary to provide an air ejection mechanism that ejects air from the portion of the base portion that is in contact with the hand. For example, a membrane mechanism may also be provided between the part of the abutment part that stores the contact with the hand and the contact with the hand, so that no dirt, sand, or backfill material accumulates, or foreign matter intrudes. [Industrial Applicability] According to the shield tail gap measuring device or shield shell of the present invention, even if the shield shell advances relative to the tunnel lining body to a point where the measuring device is installed beyond the front end of the assembled tunnel lining body, touch the hand It will not protrude toward the center axis side of the tunnel lining body from the outer periphery of the tunnel lining body, which will not become an obstacle when assembling the next tunnel lining body, and can effectively suppress the assembled tunnel lining body and shield shell The overlapping length of the rear end portions becomes longer.

10‧‧‧盾尾間隙測量裝置10‧‧‧Shield tail gap measuring device

11‧‧‧潛盾機11‧‧‧ Submersible Shield

12‧‧‧盾殻12‧‧‧Shield Shell

13‧‧‧環片13‧‧‧ ring

14‧‧‧隧道襯砌體14‧‧‧ Tunnel Lining

15‧‧‧盾尾間隙15‧‧‧shield tail gap

16‧‧‧基台部16‧‧‧ Abutment Department

16a‧‧‧底盤部16a‧‧‧Chassis

16b‧‧‧軸承壁部16b‧‧‧bearing wall

16c‧‧‧間隔部分16c‧‧‧Interval

16d‧‧‧軸承機構16d‧‧‧bearing mechanism

16e‧‧‧插通孔16e‧‧‧Plug-in hole

16f‧‧‧螺栓緊固固定孔16f‧‧‧Bolt fastening fixing hole

17‧‧‧旋轉軸部17‧‧‧rotating shaft

17a‧‧‧中央部擴徑部17a‧‧‧Central part

17b‧‧‧端部縮徑部17b‧‧‧End Reduction

17c‧‧‧中央部擴徑部17c‧‧‧Central part

17f‧‧‧端面接合孔17f‧‧‧face joint hole

18‧‧‧旋轉角感測器18‧‧‧rotation angle sensor

18a‧‧‧感測器軸18a‧‧‧Sensor shaft

19‧‧‧接觸手部19‧‧‧ touch your hand

19a‧‧‧臂本體部19a‧‧‧arm body

19b‧‧‧接合銷19b‧‧‧Joint Pin

19c‧‧‧旋轉輥接觸部19c‧‧‧Rotating roller contact

19d‧‧‧缺口面19d‧‧‧ notched surface

19e‧‧‧旋轉支持軸19e‧‧‧rotation support shaft

20‧‧‧旋轉彈推機構20‧‧‧Rotary spring push mechanism

20a‧‧‧反轉機構20a‧‧‧ Reversal mechanism

20b‧‧‧接合銷20b‧‧‧Joint Pin

20c‧‧‧配管埠20c‧‧‧Pipe port

21‧‧‧蓋體21‧‧‧ Cover

21a‧‧‧防水連接器21a‧‧‧ Waterproof connector

22‧‧‧感測器纜線22‧‧‧ sensor cable

23‧‧‧安裝凹部23‧‧‧Mounting recess

23a‧‧‧鋼製板23a‧‧‧steel plate

24‧‧‧空氣供給配管24‧‧‧Air supply piping

25‧‧‧空氣噴出孔25‧‧‧air ejection hole

26‧‧‧空氣供給套筒26‧‧‧Air supply sleeve

27‧‧‧凹槽27‧‧‧ groove

30‧‧‧旋轉切割器30‧‧‧Rotary cutter

31‧‧‧隔板31‧‧‧ bulkhead

32‧‧‧泥土壓室32‧‧‧Soil pressure chamber

33‧‧‧切割器驅動裝置33‧‧‧ Cutter driving device

34‧‧‧排土機構34‧‧‧Soil discharge agency

35‧‧‧推進千斤頂35‧‧‧advancing the jack

36‧‧‧安裝裝置36‧‧‧Installation device

40‧‧‧本體40‧‧‧ Ontology

41‧‧‧葉片41‧‧‧ Blade

42‧‧‧旋轉軸42‧‧‧Rotary shaft

43‧‧‧擋止件43‧‧‧stop

50‧‧‧盾尾間隙測量裝置50‧‧‧shield tail gap measuring device

52‧‧‧盾殻52‧‧‧Shield Shell

51‧‧‧隧道襯砌體51‧‧‧ Tunnel Lining

53‧‧‧接觸手部53‧‧‧ touch your hand

A‧‧‧部分A‧‧‧Part

A‧‧‧埠A‧‧‧Port

B‧‧‧埠B‧‧‧Port

h1‧‧‧高度h1‧‧‧ height

L1‧‧‧長度L1‧‧‧ length

L2‧‧‧長度L2‧‧‧ length

圖1係說明安裝有本發明之較佳之一實施形態之盾尾間隙測量裝置之潛盾機之構成的概略剖視圖。 圖2係說明安裝有本發明之較佳之一實施形態之盾尾間隙測量裝置之盾殻之主要部分概略剖視圖。 圖3係圖2之A部概略放大圖。 圖4係本發明之較佳之一實施形態之盾尾間隙測量裝置之立體圖。 圖5(a)係盾尾間隙測量裝置之俯視圖,(b)係沿著(a)之B-B之剖視圖。 圖6(a)、(b)係說明氣壓式旋轉致動器之反轉機構之概略剖視圖。 圖7(a)係將接觸手部以朝向盾殻之中心軸側旋動之方式彈推並檢測旋轉角之狀態的說明圖,(b)係使接觸手部朝向盾殻中心軸之相反側旋動並將其收納於基台部之高度範圍之說明圖,(c)係組裝下一個環片之狀態之說明圖,(d)係將接觸手部以朝向盾殻之中心軸側旋動之方式再次彈推並檢測旋轉角之狀態的說明圖。 圖8係使基台部之收納接觸手部之部分噴出空氣之空氣噴出機構之說明圖。 圖9(a)~(c)係說明先前之盾尾間隙測量裝置之不良狀況之主要部分概略剖視圖。FIG. 1 is a schematic cross-sectional view illustrating a configuration of a submersible shield machine equipped with a shield tail gap measuring device according to a preferred embodiment of the present invention. FIG. 2 is a schematic cross-sectional view illustrating a main part of a shield case equipped with a shield tail gap measuring device according to a preferred embodiment of the present invention. FIG. 3 is a schematic enlarged view of part A of FIG. 2. FIG. 4 is a perspective view of a shield tail gap measuring device according to a preferred embodiment of the present invention. Fig. 5 (a) is a top view of the shield tail gap measuring device, and (b) is a sectional view along B-B of (a). 6 (a) and 6 (b) are schematic cross-sectional views illustrating a reversing mechanism of a pneumatic rotary actuator. Fig. 7 (a) is an explanatory diagram of a state in which the contact hand is pushed and rotated toward the center axis side of the shield case to detect the rotation angle, and (b) is the contact hand portion toward the opposite side of the center axis of the shield case An explanatory diagram of the height range of the base part that is rotated and stored, (c) is an explanatory diagram of the state of assembling the next ring piece, and (d) is the contact with the hand to rotate toward the center axis side of the shield shell This is an explanatory diagram of a state in which the rotation angle is once again pushed and detected. FIG. 8 is an explanatory diagram of an air ejection mechanism that ejects air from a part of the base portion that contacts the hand. Figs. 9 (a) to (c) are schematic cross-sectional views of main parts illustrating the defective condition of the conventional shield tail gap measuring device.

Claims (7)

一種盾尾間隙測量裝置,其係測量保持於潛盾機之盾殻、與由在該盾殻之後部組裝之環片構成之隧道襯砌體之外周面之間的盾尾間隙之間隙量者,且 其構成為包含:基台部;旋轉軸部,其以可旋轉地支持於該基台部之狀態設置;旋轉角感測器,其檢測該旋轉軸部之旋轉角;接觸手部,其與上述旋轉軸部接合為一體且朝上述盾殻之後方側延伸設置;及旋轉彈推機構,其以使該接觸手部朝向上述盾殻之中心軸側旋動之方式對上述旋轉軸部賦予旋轉彈推力;且 上述旋轉彈推機構具備釋放旋轉彈推力而使上述旋轉軸部朝相反方向旋轉之反轉機構,且以使上述接觸手部朝上述盾殻中心軸之相反側旋動之方式使上述旋轉軸部旋轉,而能夠將上述接觸手部收納於上述基台部之高度範圍。A shield tail gap measuring device, which measures the gap between the shield shell held by the submersible shield machine and the shield tail gap between the outer peripheral surface of the tunnel lining body composed of a ring assembled at the rear of the shield shell, And its structure includes: a base part; a rotating shaft part that is rotatably supported by the base part; a rotation angle sensor that detects the rotation angle of the rotating shaft part; It is integrally connected with the rotating shaft portion and extends toward the rear side of the shield case; and a rotary spring pushing mechanism is provided to the rotating shaft portion so that the contact hand portion rotates toward the center axis side of the shield case. Rotary spring thrust; and the rotary spring thrust mechanism is provided with a reversing mechanism that releases the rotary spring thrust to rotate the rotary shaft portion in the opposite direction, and rotates the contact hand toward the opposite side of the center axis of the shield case By rotating the rotation shaft portion, the contact hand portion can be stored in a height range of the base portion. 如請求項1之盾尾間隙測量裝置,其中上述旋轉彈推機構為旋轉致動器。The shield tail gap measuring device according to claim 1, wherein the rotary spring pushing mechanism is a rotary actuator. 如請求項2之盾尾間隙測量裝置,其中上述旋轉彈推機構為氣壓式旋轉致動器。For example, the shield tail gap measuring device of claim 2, wherein the rotary elastic pushing mechanism is a pneumatic rotary actuator. 如請求項1之盾尾間隙測量裝置,其中上述接觸手部具有於臂本體部之前端具備旋轉輥接觸部之臂形狀。The shield tail gap measuring device according to claim 1, wherein the contact hand portion has an arm shape having a rotating roller contact portion at the front end of the arm body portion. 如請求項1之盾尾間隙測量裝置,其設置有使上述基台部之收納上述接觸手部之部分噴出空氣之空氣噴出機構。For example, the shield tail gap measuring device of claim 1 is provided with an air ejection mechanism that ejects air from the part of the base part that receives the contact with the hand. 一種盾殻,其係安裝有如請求項1之盾尾間隙測量裝置者,且 於配置有由組裝之環片構成之隧道襯砌體之後端部分,在內周面形成有安裝凹部,將上述盾尾間隙測量裝置以使上述接觸手部朝上述盾殻之軸向後方側延伸,且不使上述基台部自上述盾殻之內周面突出之狀態固定於該安裝凹部。A shield case is provided with a shield tail gap measuring device as claimed in claim 1, and a rear end portion of a tunnel lining body composed of an assembled ring piece is provided with a mounting recess on an inner peripheral surface thereof. The gap measuring device is fixed to the mounting recess in a state where the contact hand portion extends toward the axially rear side of the shield case and the base portion does not protrude from the inner peripheral surface of the shield case. 如請求項6之盾殻,其中上述安裝凹部於後部之周向上隔開間隔地設置於至少3個部位,且於各個上述安裝凹部固定有上述盾尾間隙測量裝置。For example, the shield case of claim 6, wherein the mounting recesses are provided at least three locations at intervals in the rear circumferential direction, and the shield tail gap measuring device is fixed to each of the mounting recesses.
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CN111795789A (en) * 2020-09-09 2020-10-20 中铁工程服务有限公司 Shield constructs experimental detection device of quick-witted center solid of revolution
CN112161581A (en) * 2020-09-22 2021-01-01 大连理工大学 Machine vision shield tail clearance dynamic measurement method considering segment end surface deflection angle
CN114111555A (en) * 2021-11-22 2022-03-01 盾构及掘进技术国家重点实验室 Mechanical shield/TBM shield tail clearance real-time measuring device and measuring method thereof

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